Small Satellite Electrical Design Interface to the STSAT2(Small satellite (1), Workshop for Space, Aeronautical and Navigational Electronics (W S A N E 2005))

概要

論文の詳細を見る
The results are presented of an investigation of the design which affect the determination of electrical interfaces for Small Satellite, STSAT2 including electrical power interface, telecommand and telemetry. The electrical power ground is designed to return single point for the spacecraft main dc voltage. But the second regulated power ground is not designed to return same primary single point, but designed to return secondary single point without sash grounding except some units for stabilized powering. There are also common grounded telemetry and telecommand interface and opto-coupled telemetry and telecommand interface for the units which are not using common ground.
社団法人電子情報通信学会の論文
2005-02-25